US4631498A - CW Laser wavemeter/frequency locking technique - Google Patents

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• • H—ELECTRICITY
  • H01—ELECTRIC ELEMENTS
  • H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
  • H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
  • H01S3/10—Controlling the intensity, frequency, phase, polarisation or direction of the emitted radiation, e.g. switching, gating, modulating or demodulating
  • H01S3/13—Stabilisation of laser output parameters, e.g. frequency or amplitude
  • H01S3/139—Stabilisation of laser output parameters, e.g. frequency or amplitude by controlling the mutual position or the reflecting properties of the reflectors of the cavity, e.g. by controlling the cavity length
  • H01S3/1398—Stabilisation of laser output parameters, e.g. frequency or amplitude by controlling the mutual position or the reflecting properties of the reflectors of the cavity, e.g. by controlling the cavity length by using a supplementary modulation of the output
• • G—PHYSICS
  • G02—OPTICS
  • G02F—OPTICAL DEVICES OR ARRANGEMENTS FOR THE CONTROL OF LIGHT BY MODIFICATION OF THE OPTICAL PROPERTIES OF THE MEDIA OF THE ELEMENTS INVOLVED THEREIN; NON-LINEAR OPTICS; FREQUENCY-CHANGING OF LIGHT; OPTICAL LOGIC ELEMENTS; OPTICAL ANALOGUE/DIGITAL CONVERTERS
  • G02F2/00—Demodulating light; Transferring the modulation of modulated light; Frequency-changing of light
• • H—ELECTRICITY
  • H01—ELECTRIC ELEMENTS
  • H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
  • H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
  • H01S3/005—Optical devices external to the laser cavity, specially adapted for lasers, e.g. for homogenisation of the beam or for manipulating laser pulses, e.g. pulse shaping
  • H01S3/0064—Anti-reflection devices, e.g. optical isolaters
• • H—ELECTRICITY
  • H03—ELECTRONIC CIRCUITRY
  • H03L—AUTOMATIC CONTROL, STARTING, SYNCHRONISATION OR STABILISATION OF GENERATORS OF ELECTRONIC OSCILLATIONS OR PULSES
  • H03L7/00—Automatic control of frequency or phase; Synchronisation

Definitions

• the disclosed invention relates in general to the comparison of an optical frequency to a radio frequency and more particularly to a technique that enables a rational ratio N/M to be established between an optical frequency and a radio frequency (RF).
• RF radio frequency
• the length L of the cavity and f 2 are adjusted so that the maximum intensities of both sidebands (i.e., at f 1 +f 2 and f 1 -f 2 ) pass through the cavity.
• a first etalon prevents the carrier frequency f 1 from entering the interferometer cavity and a pair of tuned etalons separately pass each sideband after the laser beam passes through the interferometer cavity.
• f 1 is adjusted in response to the difference in the two sideband signals and L is adjusted in response to the sum of the two sideband signals.
• this technique is not suitable for use over a broad spectral range.
• an isolator containing a quarter wave plate is included in the laser beam path between the laser and the interferometer. Because a quarter wave plate cannot produce exactly one quarter wave retardation over a wide laser frequency range, this technique is not suitable over a broad spectral range.
• the etalons would need to be gang tuned to the laser wavelength. This tuning would itself require some kind of moderate accuracy wavemeter, thereby limiting the spectral range of practical utility.
• a phase modulation technique and associated apparatus are presented that enable an optical frequency f 0 of a coherent collimated continuous wave (CW) source to be locked to a radio frequency f 1 .
• the relationship is established by use of a filter and a pair of servo loops.
• the optical beam is phase modulated with a subcarrier of frequency f 1 that is itself modulated at frequency f 2 .
• this modulation is itself pure phase modulation.
• phase is the time integral of frequency and therefore phase modulation with p(t) is identical to frequency modulation with dp(t)/dt.
• the modulated light beam passes through a filter to a detector which, in response to the incident light beam produces a detector output signal.
• Interferometers such as a Fabry-Perot interferometer (acting in either reflection or transmission mode) or a Michelson interferometer are suitable choices for the filter.
• a Fabry Perot interferometer When a Fabry Perot interferometer is utilized, it should be of the type having 3 or more mirrors so that reflections from the mirrors do not get directed back into the CW source.
• the interferometers exhibit transfer functions that are periodic functions of frequency.
• the period of the transfer function is a fundamental frequency f f determined by the speed of light and the dimensions of the interferometer. At points of amplitude symmetry, the curve of the phase shift introduced by the transfer function is antisymmetric.
• a first phase synchronous amplifier is responsive to the detector output signal and a first reference signal to produce a first control signal.
• a second phase synchronous amplifier is responsive to the detector output signal and a second reference signal to produce a second control signal
• the first control signal is utilized in a first servo loop to lock optical frequency f 0 to (N+1/2) times f f where N is a large integer
• the second control signal is utilized in a second servo loop to lock radio frequency f 1 to (M+1/2) times f f where M is a small integer
• This also locks the frequency f 0 to f 1 by setting the ratio of f 0 /f 1 equal to (2N+1)/(2M+1).
• This relationship can be utilized in conjunction with a stable source of radio frequency f 1 to stabilize the optical frequency f 0 or, conversely, can be used with a stable source of optical frequency f 0 to stabilize the source of radio frequency f 1 .
• the first and second reference signals can be viewed as a pair of reference vectors.
• the phase synchronous integrations performed by the phase synchronous amplifiers measure the amount of each of these two vectors contained in the detector output signal.
• each control signal is a measure of the amount of its associated reference vector contained in the detector output signal.
• the first reference signal is chosen so that the first control signal goes to zero as f 0 -(N+1/2)*f f approaches zero, but does not go to zero as f 1 -(M+1/2)*f f goes to zero.
• the second reference signal is chosen so that the second control signal goes to zero as f 1 -(M+1/2)*f f goes to zero, but does not go to zero as f 0 -(N+1/2)*f f goes to zero.
• the first and second servo loops are effective to lock f 0 to (N+1/2)*f f and f l to (M+1/2)*f f , respectively.
• both of the reference signals and their negatives are utilized in sequence as phase reference inputs to the first phase synchronous amplifier to step the ratio f 0 /f f from N+1/2 to N+P+1/2.
• the ratio f 0 /f f is varied by varying only one of f 0 and f f .
• f 1 /f 2 is measured at each of these ratios of f 0 /f f .
• the value of M can be determined by a number of methods including: (1) a rough knowledge of f 1 and the dimensions of the cavity; or (2) additional measurements of frequencies when M is stepped between a pair of values in a manner equivalent to that just discussed in which the value of N is stepped between a pair of values.
• first order frequency dispersion in such elements as the mirrors in the interferometer will introduce a delay D that is typically unknown.
• This delay produces a shift in the servo locking condition of loop 2 such that (N+1/2)/f 0 still equals 1/f f , but now (M+1/2)/f 1 is equal to D+1/f f . Therefore, (M+1/2)*(1/f 1 '-1/f 1 ) is still equal to P/f 0 independent of the value of D. Therefore, this method for determining N is not affected by the unknown delay D. N is affected in just the right way so that the determined value of N corrects the calculated f 0 for the effects of D.
• FIG. 1 is a block diagram of a circuit for indirectly setting a first frequency to a fixed multiple of a second frequency.
• FIGS. 2A is a spectral distribution of an amplitude modulated signal.
• FIG. 2B is a spectral distribution of a phase modulated signal.
• FIG. 2C is a spectral distribution of a signal that is both phase and amplitude modulated.
• FIG. 2D is a spectral distribution of a signal that is phase modulated by a signal that is itself phase modulated.
• FIGS. 3 and 4 illustrate the effect of the transfer function of a Michelson interferometer on a signal of the type presented in FIG. 2D.
• FIG. 5 shows the amplitude and phase components of the transfer function of a Michelson interferometer.
• FIGS. 6 and 7 illustrate the effect of the transfer function of a Fabry Perot interferometer on a signal of the type presented in FIG. 2D.
• FIG. 8A is a table of the amplitude of a control signal produced by a phase synchronous amplifier in response to four different phase signals.
• FIG. 8B is a simplified version of the table of FIG. 8A emphasizing the functional dependence of the entries in the table.
• FIG. 1 a circuit suitable for locking a signal of radio frequency f 1 to a signal of optical frequency f 0 .
• a coherent continuous wave source of collimated light such as laser 11, produces an optical beam 12 of frequency f 0 that passes through an electrooptic phase modulator 13 to phase modulate the optical beam.
• Phase modulator 13 is responsive to the output signal from a voltage controlled oscillator (VCO) 14
• VCO voltage controlled oscillator
• a bias signal produced by a loop filter 15 is added in an adder 16 to a signal of radio frequency f 2 produced by an RF source 17. The sum of these two signals is applied to the control input of VCO 14 so that the RF component introduces frequency modulation of the VCO frequency and the bias signal from loop filter 15 adjusts the average VCO frequency.
• beam 12 is phase modulated by a modulation signal that itself is frequency modulated at frequency f 2 .
• the choice of bias signal is made to lock the average frequency f 1 of the VCO to M+1/2 times a fundamental frequency f f of an interferometer, where M is a small integer.
• phase modulated signal A*cos[2 ⁇ f c t+(2B/A)*sin(2 ⁇ f m t)] to first order in B is equal to
• the spectral distribution for the amplitude modulated signal is shown in FIG. 2A and the spectral distribution for the phase modulated signal is shown in FIG. 2B. In both of these figures, the spectral distribution shows the carrier frequency at f c plus a pair of side bands at f c ⁇ f m . In FIG. 2C is shown the spectral distribution for a signal of frequency f c that is both amplitude and phase modulated at frequency f m .
• phase of the upper side band minus the phase of the carrier must at all times be equal, mod 2 ⁇ , to ⁇ plus the phase of the carrier minus the phase of the lower side band; and (ii) the amplitude of the upper side band must equal the amplitude of the lower side band.
• FIG. 2D is shown the spectral distribution for optical beam 12 after passing through modulator 13.
• Beam 12 contains a carrier component 21 at frequency f 0 which is phase modulated as a result of sideband clusters 22-24 and 25-27.
• Each of the sideband clusters has the form of FIG. 2B because they each represent the phase modulated signal applied by VCO 14 to the control input of modulator 13. If this beam were incident on a detector, the detector signal would be constant because the modulation of the beam is pure phase modulation. However, if the relationship between the components of the beam are disturbed in a way that violates either criterion (i) or criterion (ii) above for pure phase modulation, then the detector signal will not be constant.
• the relationship between the components of phase modulated optical beam 12 are disturbed by passing the beam through a filter before detecting the beam with a detector 111.
• the transfer function T*e -ip disturbs the relationship between the components that produces a purely phase modulated signal.
• the Michelson interferometer (consisting of beam splitter 18, fixed cube corner 19 and translatable cube corner 110) functions as a filter having properties that enable the optical frequency f 0 to be locked to the average frequency f 1 produced by VCO 14.
• FIGS. 3 and 4 are shown, as a function of frequency, the amplitude T (curves 31 and 41) and phase p (curves 32 and 42) of the transfer function of the Michelson interferometer.
• Both T and p are periodic with a period c/L where c is the speed of light in the interferometer and L is the excess path length for the portion of the beam that travels to cube corner 19 over the path length for the portion of the beam that travels to cube corner 110.
• curve p is antisymmetric about that point and curve T is symmetric about that point.
• Curves 33-35 and 43-45 show the components of the optical beam before passage through the interferometer. After passage through the interferometer, the resulting amplitude curve for the spectral distribution of the optical beam is the product of curves 33-35 with curve 31 and the product of curves 43-45 with curve 41. Curves 32 and 42 show the amount of phase shift introduced into each of the components as a function of the frequency of each component. It should be remembered that the negative amplitude of component 25 is really an indication that the phase difference between components 25 and 21 is 180 degrees out of phase with respect to the phase difference between components 21 and 22.
• a first servo loop containing a first phase synchronous amplifier 112, a first loop filter 113 and a translator 114 are utilized to adjust f f so that f 0 is equal to a half integral multiple N+1/2 times f f .
• Amplifier 112 is responsive to the output of detector 111 and to a first reference signal to produce a first control signal proportional to the filtered product of the first reference signal and the detector output signal.
• the loop filter has a transfer function that makes the first servo loop stable and of order 1 or higher (i.e., at least one integration in the open loop transfer function).
• a translator 114 translates cube corner 110 in a direction that varies the distance of cube corner 110 from beam splitter 18. This translation varies the fundamental frequency f f of the interferometer, thereby altering the ratio between f 0 and f f .
• the position of the cube corner along the direction of translation is proportional to the output signal from loop filter 113.
• a suitable translator includes in series a motor and a piezoelectric crystal. The motor enables slow long translations to be performed and the piezoelectric crystal provides a fast short response for the first servo loop.
• the first control signal is chosen to approach zero as f 0 /f f approaches N+1/2 where N is an integer so that translation of cube corner 110 stops when the half integral ratio between f 0 and f f is established.
• a second servo loop containing a second phase synchronous amplifier 115, a second loop filter 15 and an adder 16 are utilized to lock f 1 to a half integral multiple M+1/2 of f f .
• M will be a small number on the order of 1-10 whereas N will be several orders of magnitude larger to enable an optical frequency (typically on the order of 500 TeraHertz) to be locked to a radio frequency (typically on the order of 500 MegaHertz).
• Amplifier 115 is responsive to the output of detector 111 and to a second reference signal to produce a second control signal proportional to the filtered product of the second reference signal and the detector output signal.
• the loop filter has a transfer function that makes the second servo loop stable and of order 1 or higher (i.e., at least one integration in the open loop transfer function).
• the application of this servo output signal to VCO 14 controls the average frequency f 1 of the VCO, thereby altering the ratio between f 1 and f f .
• the second control signal is chosen to approach zero as f 1 /f f approaches M+1/2 where M is an integer so adjustment of the average VCO frequency stops when the half integral ratio between f 1 and f f is established.
• each servo loop will establish a stable lock condition only when the control signal becomes zero.
• the radio frequency f 1 is indirectly locked to optical frequency f 0 by separately locking some multiple L of f f to f 0 and f 1 to some multiple K of f f .
• the first control signal goes to zero as f 0 /f f approaches L, but does not go to zero as f 1 /f f approaches K; and (2) the second control signal goes to zero as f 1 /f f approaches K, but does not go to zero as f 0 /f f approaches L.
• condition (1) holds, but condition (2) does not hold, then when the first servo loop is in a lock state, both control signals are zero regardless of whether the second servo loop is in a lock state. This prevents the second servo loop from adjusting f 1 /f 0 to a lock state condition.
• the output signal from detector 111 is proportional to the intensity I of beam 12 at detector 111.
• the intensity is itself equal to S*S* where S is the complex amplitude of the optical signal and S* is the complex conjugate of S.
• This product of S and S* contains cross products between the components of the optical signal.
• Detector 111 functions as an integrator that averages the optical signal over a time that is long compared to 1/f 0 , but is short compared to 1/f 1 and 1/f 2 . Therefore, components of I at optical frequencies average to zero, thereby leaving only components at linear integral sums of f 1 and f 2 .
• the control signals are each a linear function of the detector signal so that control signals that satisfy criterion (1) of the previous paragraph can be generated by determining which of the components of the detector output signal vanish as f 0 /f f approaches L, but do not vanish as f 1 /f f approaches a half integer.
• the optical beam is purely phase modulated when f 0 and f 0 ⁇ f 1 are located at extrema (e.g., as for curves 33 and 43 in FIGS. 3 and 4, respectively) so that the output signal from the detector is constant under such conditions. Therefore, all components of the detector output signal, other than its DC component, are zero when this condition is established.
• f 0 and f 1 are each at some extremum of T and therefore are each some integral multiple of f f /2.
• K and L are both some integral multiple of 1/2.
• Curves 34 and 35 represent the case where K is held at 1/2, but f 0 is varied a small amount d' away from (N+1/2)*f f .
• the detector output signal has components at f 1 and at f 1 ⁇ f 2 .
• the component of the detector output signal at f 1 arises from the cross terms in S*S* of peak 22 with peak 21 and peak 25 with peak 21.
• peaks 22 and 25 are clipped equally so that criterion (ii) for pure phase modulation at frequency f 1 continues to hold. However, condition (i) is violated because components 21, 23 and 25 pick up phase shifts of minus 90 degrees plus p 1 , p 1 and p 1 , respectively.
• the component of the detector output signal at f 1 +f 2 arises from the cross terms of component 23 with 21 and component 26 with 21.
• the component of the detector output signal at f 1 -f 2 arises from the cross terms of component 24 with 21 and component 27 with 21.
• the same reasoning as used to show the existence of a component at f 1 shows that there are also components in the detector output signal at f 1 ⁇ f 2 .
• each of these components are nonzero even when f 1 is an integral multiple of f f /2, each of these components separately or in linear combination are suitable for use as the first reference signal.
• the linear combination of these components representing the output signal from VCO 14 is a suitable choice. Therefore, in the circuit of FIG. 1, the output of VCO 14 is connected to the first phase input of the phase selector to provide the first reference signal to the first phase synchronous amplifier.
• the component of the detector output signal at f 2 arises from the cross terms of component 23 with 22, component 24 with 22, component 26 with 25 and component 27 with 25.
• the cross term of component 23 with 22 cancels the cross term of component 27 with 25 and, likewise, the cross term of component 24 with 22 cancels the cross term of component 26 with 25. Therefore, for K held at 1/2, there is no component of the detector output signal at f 2 .
• This same reasoning in regard to FIG. 4 shows that when L is held at N+1/2, the only component in the detector output signal, other than the DC component, is the component at f 2 . Therefore,
• the output of signal source 17 is utilized to provide the second reference signal to the second phase synchronous amplifier.
• the first and second servo loops independently function to lock the multiple N+1/2 of f f to f 0 and to lock f 1 to the multiple 1/2 of f f .
• the first servo loop will function to lock L times f f to f 0 whenever L is either an even or an odd integral multiple of 1/2.
• the first servo loop will lock L*f f to f 0 only if f 1 is an odd multiple of f f /2 (i.e., (M+1/2)*f f ). Therefore, K must be an odd multiple of 1/2.
• the first servo loop will function with f 0 at either a maximum or a minimum of curve 31 (i.e., for f 0 either an even or an odd multiple of f f ), by setting f 0 to a minimum, the carrier component in the detector output signal is suppressed, thereby increasing the signal to noise ratio for both control signals Therefore, it is advantageous to select L to be an odd integral multiple of 1/2.
• the transmission curves 31, 32, 41, and 42 are for the case of a Michelson interferometer having equal splitting at beam splitter 18 (i.e., the electric field amplitude in the long path between splitter 18 and cube corner 19 is equal to the electric field amplitude in the short path between splitter 18 and cube corner 110).
• the transmission curves are altered
• FIG. 5 are a set of curves for both T and p for various ratios of splitting. These curves present, as a function of frequency, the ratio between: (1) the electric field at detector 111 when light from both the short and long paths are combined as input to the detector; and (2) the electric field at detector 111 when the short path is blocked so that only light from the long path is provided as input to the detector.
• the values 0.6-1.4 represent the ratio of: (1) the amplitude of the electric field at cube corner 110 to the amplitude of the electric field at cube corner 19. These curves show that the symmetries of the amplitude and phase curves continue to hold for unequal beam splitting so that interferometers can be used which do not have equal beam splitting.
• FIGS. 6-8 are shown transfer function curves for a Fabry Perot interferometer operating in reflection mode that are analogous to the curves presented in FIGS. 3-4 for a Michelson interferometer. These curves exhibit the same type of symmetry as do the curves for the Michelson interferometer--namely, both the transmission curves have a common period and, at each point of symmetry of the amplitude curve, the phase curve is antisymmetric. Therefore, the analysis above for a circuit utilizing a Michelson interferometer is also applicable to a circuit utilizing a Fabry Perot interferometer.
• the curves for the Fabry Perot interferometer have sharper transitions than do the curves for the Michelson interferometer, a larger control signal is produced for a given amount of detuning from the lock conditions. This increases the signal to noise ratio, therby making the use of the embodiment using a Fabry Perot interferometer more advantageous for applications in which the radio frequency f 1 is used to stabilize the optical frequency f 0 or conversely.
• the Fabry Perot interferometer in order to have high finesse mirrors, the mirrors have many layers of coating which introduce a larger dispersion than is introduced in a Michelson interferometer.
• the Fabry Perot interferometer does not have high finesse over a broad spectral range. Therefore, a Michelson interferometer is more suitable for use in a circuit utilized as a wave meter.
• f 0 the values of M, f 1 , f 2 and N must be determined.
• M can ve determined by knowledge of the approximate value of f 1 and the path difference between the long and short paths of the interferometer.
• f 2 is a radio frequency and therefore is directly measurable.
• N and f f are determined by measuring the ratio f 1 /f 2 for f 0 /f f equal to N+1/2 and then again for f 0 /f f equal to N+Q+1/2 where Q is known.
• a phase selector 123 is included to select among four possible signals for use as the first reference signal applied to the first phase synchronous amplifier 112.
• the four choices of signal, applied to phase selector 123 at inputs 116-119, are: (1) the output signal of VCO 14; (2) the output signal of RF source 17; (3) minus the output signal of VCO 14; and (4) minus the output signal of RF source 17. These four choices are referred to herein as the first phase signal, the second phase signal, the third phase signal and the fourth phase signal, respectively.
• These four choices are utilized sequentially to step the lock point of the first servo loop from an initial value (N+1/2)*f f to a final value of (N'+1/2)*f f . The manner in which this stepping occurs can be seen by reference to FIGS. 8A and 8B.
• FIG. 8A is presented a table showing the amplitude of the first control signal that results for each of the four choices of phase signal.
• I 0 is a proportionality constant determined by the detector and the first phase synchronous amplifier
• P 0 is the maximum phase swing produced by electrooptic phase modulator 13
• d/2 ⁇ equals f 1 -(M+1/2)*f f
• E is the amplitude of the sinusoidal change in the output frequency from VCO 14.
• the second phase synchronous amplifier 115 is designed to produce a negative value for d when the second servo loop is disabled.
• a gate 120 is included to enable the second servo loop to be controllably disabled.
• Phase selector 123 and gate 120 are responsive to signals from a controller 121 to control the sequential use of the phase signals and to calculate N and f o .
• FIG. 8B the table of FIG. 8A has been rewritten to stress the qualitative behavior of the control signal for each of the choices of input phase signal when the second servo loop is disabled--namely, the multiplicative constants of FIG. 9A have been removed, but the sign of each term has been retained.
• the second servo loop is disabled by gate 120. Since the first servo loop is still enabled, f 0 remains equal to (N+1/2)*f f .
• Phase selector 123 next applies the second phase signal. This produces a positive control signal that adjusts the position of cube corner 110 to vary f f until f 0 is equal to (N+3/4)*f f .
• the subsequent application of the third phase signal followed by application of the fourth phase signal and then again the first phase signal successively adjusts f f to produce successively the ratios N+1, N+5/4, and N+1+1/2 for f 0 /f f .
• the second servo loop is then enabled by gate 120 so that f 1 is locked to (M+1/2)*f f and therefore can be measured.
• the first mode is the measurement mode where f 0 /f f is alternately stepped back and forth between N+1/2 and N+Q+1/2 with f f being measured at both of these points.
• a frequency counter counts the number of cycles of the VCO that occur in J cycles of signal source 17. By counting over an integral number of cycles of source 17, the effect of the periodic variation of the VCO frequency is removed. Therefore, the number of cycles counted divided by J is equal to f 1 /f 2 . Since J, M and f 2 are known, f f is determined for both the ratio N and N' for f 0 /f f .
• the VCO frequency is locked to the laser frequency
• this same technique can be utilized to lock the laser frequency to the VCO frequency.
• the output of first loop filter 113 would be applied to laser 11 to adjust its frequency and the output of second loop filter 15 would be applied to cube corner 110 to adjust the frequency f f .
• This version of the technique enables a laser to be stabilized by a stable RF source, thereby providing an accurate frequency source at optical frequencies.
• beam 12 could be modulated with a signal that is purely amplitude modulated or is partly phase modulated and partly amplitude modulated.
• the loop 2 phase reference would then be sin 2 ⁇ (f 1 -f 2 )t.
• Phase 1 through phase 4 for the phase selector would then be sin(2 ⁇ f 2 t), sin(2 ⁇ (f 1 -f 2 )t), -sin(2 ⁇ f 2 t), and -sin(2 ⁇ (f 1 -f 2 )t), respectively.

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Abstract

Description

A*cos(2πf.sub.c t)+B*cos[(2πf.sub.c +2πf.sub.m)t]+B*cos[(2πf.sub.c -2πf.sub.m)t]

A*cos(2πf.sub.c t)+B*cos[(2πf.sub.c +2πf.sub.m)t]-B*cos[(2πf.sub.c -2πf.sub.m)t]

N+Q+1/2=f.sub.0 /f.sub.f2 and

N+1/2=f.sub.0 /f.sub.f1.

f.sub.0 =Q*f.sub.f1 *f.sub.f2 /(f.sub.f1 -f.sub.f2) and

N=Q*f.sub.f2 /(f.sub.f1 -f.sub.f2)-1/2.

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Cited By (92)

Citations (4)

• 1985
  • 1985-04-26 US US06/727,457 patent/US4631498A/en not_active Expired - Lifetime

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